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2. Absolute Radiation Measurement During Planetary Entry in the NASA Ames Electric Arc Shock Tube Facility.
- Author
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Cruden, Brett A.
- Subjects
- *
ATMOSPHERIC entry of space vehicles , *RADIATION measurements , *PLASMA gases , *SHOCK tubes , *PLANETARY atmospheres , *ULTRAVIOLET radiation , *VACUUM - Abstract
During planetary entry, a shock-heated plasma that imparts significant heating to the structure is formed in front of the space vehicle. At high velocities, a significant portion of that energy transfer originates from radiation from the shock-heated plasma. Shock tubes are capable of simulating the high velocity and low density conditions typical of planetary entry and thus are able to recreate the radiative environment encountered by spacecraft. The Electric Arc Shock Tube (EAST) at NASA Ames Research Center is one of the few shock tubes in the world that is capable of reaching the high velocities that are necessary to study more extreme entry conditions. The EAST is presently being utilized to simulate radiation in a variety of planetary atmospheres. It is presently the only facility in which radiation originating in the vacuum ultraviolet is being quantified. This paper briefly describes recent tests in the EAST facility relevant to Earth, Mars, and Venus entry conditions, and outlines the issues in relating ground test data to flight relevant condition via predictive radiation simulations. [ABSTRACT FROM AUTHOR]
- Published
- 2011
- Full Text
- View/download PDF
3. Ion Thruster Modeling: Particle Simulations and Experimental Validations.
- Author
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Wang, Joseph, Polk, James, and Brinza, David
- Subjects
- *
SPACE vehicles , *PLASMA gases - Abstract
This paper presents results from ion thruster modeling studies performed in support of NASA's Deep Space 1 mission and NSTAR project. Fully 3-dimensional computer particle simulation models are presented for ion optics plasma flow and ion thruster plume. Ion optics simulation results are compared with measurements obtained from ground tests of the NSTAR ion thruster. Plume simulation results are compared with in-flight measurements from the Deep Space 1 spacecraft. Both models show excellent agreement with experimental data. [ABSTRACT FROM AUTHOR]
- Published
- 2003
4. FOREWORD.
- Author
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Drake, James F. and Davidson, Ronald C.
- Subjects
- *
PHYSICS , *PHYSICAL sciences , *PLASMA gases , *INTERSTELLAR medium , *PLASMA turbulence , *CONFERENCES & conventions - Abstract
Introduces this issue as a special issue which is a collection of articles based on invited presentations at the 41st Annual Meeting of the Division of Plasma Physics (DPP) of the American Physical Society held in Seattle, Washington, in November 1999. Details of the program which involved several papers and a mini-conferences on Turbulence in the Interstellar Medium and Solar Wind, Plasma Propulsion Physics, Dusty Plasmas, and Computational Studies of Complexity in Turbulent Plasma; Coverage of a broad variety of research in plasma physics and highlighting of areas of intense interest and investigation, such as the basic physics of waves, instabilities, turbulence and transport and the properties of non-neutral plasmas and matter under very high pressures; Details of tutorial papers and presentations which are meant to be understood by non-experts.
- Published
- 2000
5. Trends in plasma conditions inferred from an analysis of x-ray data from high wire-number, Z-pinch load implosions.
- Author
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Whitney, K. G., Pulsifer, P. E., Apruzese, J. P., Thornhill, J. W., Davis, J., Chong, Y. K., Sanford, T. W. L., Mock, R. C., and Nash, T. J.
- Subjects
- *
X-rays , *PLASMA gases - Abstract
An analysis of x-ray data from two series of Z-pinch shots taken on the short current-risetime Saturn accelerator at Sandia National Laboratories [Proceedings of 6th International IEEE Pulsed Power Conference, Arlington, VA, edited by P. J. Turchi and B. H. Bernstein (IEEE, New York, 1987), p. 310] is presented. In one series, the array radius was held constant and the array mass was varied; in the other series, the array mass was held constant and its radius varied. In both sets of experiments, large wire-number loads (N>=93) of aluminum were used in contrast to earlier small wire-number aluminum array experiments on Saturn where N≤42. Average electron temperatures and ion densities were inferred from the data. In addition, from the measured size of the emission region of K-shell x rays and from the inferred ion density, a fraction of the total array mass that participated in the K-shell emission was inferred and found to be directly correlated to the K-shell yields that were measured. This paper also demonstrates that the yields varied as a function of array mass and radius in much closer agreement with predictions [J. Appl. Phys. 67, 1725 (1990)] than had been observed in the earlier small wire-number experiments. Thus, a serious misperception that the reason for the early disagreement was in the calculations and not in the experiments is corrected. These predictions were made using one-dimensional (1D) magnetohydrodynamics calculations. The density and temperature trends inferred from the data analysis are well-behaved and consistent with the 1D calculations. This data analysis confirms the importance of achieving uniform plasma initial conditions and implosion symmetry when comparing computer code calculations with experiment. When the wire number of an array load is increased, a more uniform shell of plasma is calculated initially as the wires explode and, as the plasma stagnates on axis, the x-ray powers and yields are found experimentally to appro... [ABSTRACT FROM AUTHOR]
- Published
- 2001
- Full Text
- View/download PDF
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